Title:
ACTUATOR FOR CONTROLLING LANDING GEAR AND CONTROL METHOD THEREOF
Document Type and Number:
Japanese Patent JP2016222132
Kind Code:
A
Abstract:
PROBLEM TO BE SOLVED: To prevent breakage of an airframe by lowering a preload to be generated when a landing gear is brought into contact with a second stopper.SOLUTION: An actuator for controlling a landing gear and a control method thereof are a configuration and a method for preventing breakage of an airframe (20), etc. by reducing a preload to be generated by bringing a landing gear (9) provided at the tip of a link mechanism (8) into contact with a second stopper (11) by an actuator (1), and holding torque of an electromagnetic brake (2A) of a motor (2) with the electromagnetic brake of the actuator (1).SELECTED DRAWING: Figure 1
Inventors:
KITAHARA KAZUHITO
Application Number:
JP2015111107A
Publication Date:
December 28, 2016
Filing Date:
June 01, 2015
Export Citation:
Assignee:
TAMAGAWA SEIKI CO LTD
International Classes:
B64C25/24; B64C25/44
Attorney, Agent or Firm:
Michiharu Soga
Kajinami order
Masahiro Taguchi
Ichiro Oi
Kazuhiro Mitsunaga
Kanayama Asuka
Kajinami order
Masahiro Taguchi
Ichiro Oi
Kazuhiro Mitsunaga
Kanayama Asuka